| タイトル | Design considerations for the airframe-integrated scramjet |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740004335 |
| 著者（英） | Henry, J. R.; Anderson, G. Y. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1973-12-01 |
| 言語 | eng |
| 内容記述 | Research programs at the NASA Langley Research Center on the development of airframe-integrated scramjet concepts (supersonic combustion ramjet) are reviewed briefly. The design and performance of a specific scramjet configuration are examined analytically by use of recently developed and substantiated techniques on boundary-layer development, heat transfer, fuel-air mixing, heat-release rates, and engine-cycle analysis. These studies indicate that the fixed-geometry scramjet module will provide practical levels of thrust performance with low cooling requirements. Areas which need particular emphasis in further development work are the combustor design for low speeds and the integrated nozzle design. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 74N12448
NASA-TM-X-2895
L-8152 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/196629 |
